Vasantha, R (1994) Rolled-up wake field behind aircraft configurations. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
The panel code which accounts for the effects of13; wake behind aircraft configurations has been made13; the new CONVEX super computer of GM MACS .the rolled up operational on DLR aircraft configuration result.. are reproduced and are shown in Figs. I and 2. Using the present panel code results for LTA with rolled-up wake field for different angles of attack and are presented in this report .Vl aircraft are obtained and are presented in this report.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Panel method;Aircraft wake;Wake relaxation;Trailing vorticies |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Mr. N A |
| Date Deposited: | 02 Jun 2006 |
| Last Modified: | 24 May 2010 09:42 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1526 |
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